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Finite element computation of compressible flows with the SUPG formulationFinite element computation of compressible Euler equations is presented in the context of the streamline-upwind/Petrov-Galerkin (SUPG) formulation. The SUPG formulation, which is based on adding stabilizing terms to the Galerkin formulation, is further supplemented with a shock capturing operator which addresses the difficulty in maintaining a satisfactory solution near discontinuities in the solution field. The shock capturing operator, which has been derived from work done in entropy variables for a similar operator, is shown to lead to an appropriate level of additional stabilization near shocks, without resulting in excessive numerical diffusion. An implicit treatment of the impermeable wall boundary condition is also presented. This treatment of the no-penetration condition offers increased stability for large Courant numbers, and accelerated convergence of the computations for both implicit and explicit applications. Several examples are presented to demonstrate the ability of this method to solve the equations governing compressible fluid flow.
Document ID
19930045777
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Le Beau, G. J.
(NASA Johnson Space Center Houston, TX, United States)
Tezduyar, T. E.
(Minnesota Univ. Minneapolis, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Advances in finite element analysis in fluid dynamics - 1991; Proceedings of the Symposium, ASME Winter Annual Meeting, Atlanta, GA, Dec. 1-6, 1991 (A93-29773 10-34)
Publisher: American Society of Mechanical Engineers
Subject Category
Aerodynamics
Accession Number
93A29774
Funding Number(s)
CONTRACT_GRANT: NSF MSM-87-96352
CONTRACT_GRANT: NAG9-449
Distribution Limits
Public
Copyright
Other

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